As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING THE 1ST 200 HR INSPECTION A CRACK WAS DISCOVERED IN THE ELEVATOR SKIN COLOLATED WITH A STATIC WICK RIVET. STATIC WICK BASE REMOVED, PATCH INSTALLED IAW SRM 55-00-00 AND 51-00-00. STAIC WICK BASE RE-INSTALLED. SUBSEQUENT INSPECTION AT +10HRS HAS NOT REVEALED ANY ADDITIONAL CRACKING. MFG HAS BE NOTIFIED.